(2) ASME B16.47 flanges now use updated pressure ratings for Group 1.18 materials from the B16.47-2017 standard.
(3) UG-14 Rods and Bars: The following new deficiencies are issued for parts machined from rod or bar material:
The switch Use UG-14(b)(3) stress reduction for rod or bar material is now available in Set Mode Options -> Calculation -> General 2 -> Calculation Options. This switch can also be turned on by entering the Material Properties dialog from the component dialog that is machined from rod or bar.
(4) UG-39(b)(3): The ligament check now uses the diameter as defined in UG-34.
(5) UG-44: Subparagraph notations revised.
(6) UG-44(b): The rules for evaluating external loads for flanged joints with welding neck flanges are now included as UG-44(b). The option switch Use UG-44(b) (flange loading moment factor) now replaces Use Code Case 2901 (flange loading moment factor) in Codes -> ASME -> Options.
(7) Figure UW-16.1: Sketch (p-2) weld sizing rules for studding outlets attached by full penetration weld are now available.
(8) UCS-66(c): ASME B16.5/B16.47 flanges are now exempt from impact testing when minimum design metal temperature is not colder than -20°F (-29°C) and they are produced to a fine grain practice and supplied in heat treated condition. ASME B16.5/B16.47 flanges supplied in the as-forged condition are exempt from impact testing when minimum design metal temperature is not colder than 0°F (-18°C). The option switch Supplied in heat treated condition & produced to fine grain practice is now available in the Select ASME B16.5/16.47 Flange dialog.
(9) Figure UCS-66 and UCS-66M: SA-105 forged fittings and flanges are now in Curve A if in as-forged condition and Curve B if produced to fine grain practice and normalized. SA/GB 713 Grade Q345R is added to Curve B if not normalized and Curve D if normalized.
(10) UCS-79(d): Subparagraph notations revised.
(11) UNF-56: Postweld heat treatment messages now reference the redesignated paragraphs to reflect UNF-56(c) deletion.
(12) UNF-79 and UHA-44: The minimum annealing time stated for post fabrication heat treatment deficiencies is updated.
(13) Table UNF-79: Post fabrication strain limits are now updated for new and existing materials listed for lower and higher temperature ranges.
(14) Table UHA-23: The materials database now considers SA/EN 10028-7 materials as SA-240 materials with the updated grades from table UHA-23.
(15) Table UHA-32-2: The following alloys are now exempt from postweld heat treatment: UNS S40910, S40920, S40930, S40935, S40936, S40945, S40975, S40977, S43932, and S43940.
(16) UHA-32 - Tables UHA-32-3 and UHA-32-7: A cautionary deficiency has been added if postweld heat treatment is applied to P-No. 8 materials.
(17) UHA-51(d)(3): The nominal thickness is defined for plates, pipes, and other product forms for determining if a material is exempt from impact testing.
(18) Table UHT-56: SA-553 III is now included in postweld heat treatment thickness limit checks.
(19) Appendix 2-9(d): Rigidity calculations are no longer required and may now be deactivated for split loose flanges through the Flange Type dialog.
(20) Appendix 46: The rules for designing a Section VIII, Division 1 pressure vessel to Division 2 rules are now included as Appendix 46. The option switch Use Appendix 46 (Use Div 2 rules) now replaces Use Code Case 2695 (Use Div 2 rules) in Codes -> ASME -> Options, and in component dialogs where the switch was previously available.
(21) U-Forms: Signed replaces Name for the Authorized Inspector on Forms U-4 and U-5. [68969]
The switch Use 3.2.5.2(b)(3) stress reduction for rod or bar material is now available under Action -> Set Mode Options -> Calculation -> General 2 -> Calculation Options. This switch can also be turned on by entering the Material Properties dialog from the component dialog that is machined from rod or bar.
(10) 3.11.2.4: The option to specify ASME B16.47 flanges produced to fine grain practice is now available.
(11) 4.1.5.3: A pressure load factor is now available in Set Mode Options -> General 1 -> Pressure load factor for wind, seismic, and vortex shedding load cases.
(12) 4.3.10.2: A deficiency is now reported when the cone half apex angle is greater than 60 degrees. Additionally, the principal stress S3 is now always zero.
(13) 4.4.2: The method of determining the design factor FS is updated.
(14) 4.4.4: Equations starting at 4.4.4 are now renumbered to reflect the deletion of equation 4.4.3.
(15) 4.4.5 and 4.4.7 : Equations for calculating predicted inelastic buckling stress are removed.
(16) 4.4.12.2(b), 4.4.12.2(c), 4.4.12.2(d): The inelastic buckling stress from 4.4.3 is used.
(17) 4.5.13: A deficiency is now reported when a nozzle limit of reinforcement overlaps a structural discontinuity.
(18) 4.15.3.4: The allowable shear stress for cylinders is updated.
(19) 4.16.6.1: The Cus factor is now removed from flange design bolt load calculations for Wgs.
(20) 4.16.8(d): Rigidity calculations are no longer required and can now be deactivated for split loose flanges through the Flange Type dialog.
(21) 4.16.12: The rules for evaluating external loads for flanged joints with welding neck flanges are now included as 4.16.12. The option switch Use 4.16.12 (flange loading moment factor) now replaces Use Code Case 2901 (flange loading moment factor) in Codes -> ASME -> Options.
(22) 6.1.2.5: The minimum annealing time stated for post fabrication heat treatment deficiencies is updated.
(23) 6.4.6: Postweld heat treatment messages now reference the redesignated paragraphs to reflect 6.4.6.2 deletion.
(24) 8.1.3.1: Vessels designed for vacuum or partial vacuum now use the test load factor from Table 4.1.3.
(25) 8.2: The test equation factor is updated.
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